thrustClass

P17733

predicate

Indicates the classification of an engine or propulsion system based on the amount or category of thrust it can produce.

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All labels observed (3)

Label	Occurrences
thrustClass canonical	201
thrustCategory	3
thrustComparedToBlock1	1

Description generation (PDg)

The one-sentence description above was generated by prompting gpt-5.1 with the predicate name and this instruction.

Instruction

Given a predicate that represents a relationship or action between entities, generate a one-sentence description explaining its meaning.  
# Instructions
Focus on describing the relationship, not the entities themselves. 
# Response Format
Begin the description with \' Indicates...\'

Input

Predicate: thrustClass

Generated description

Indicates the classification of an engine or propulsion system based on the amount or category of thrust it can produce.

Sample triples (205)

Subject	Object
Pratt & Whitney F135 engine surface form: Pratt & Whitney F135	over 40,000 pounds of thrust with afterburner ⓘ
Pratt & Whitney F117-PW-100	40,000–50,000 lbf ⓘ
Raptor	high-thrust engine ⓘ
Block 1B	similar liftoff thrust to SLS Block 1 via predicate surface "thrustComparedToBlock1" ⓘ
Walter HWK 109-509	approximately 1,500 kgf ⓘ
Walter HWK 109-509	approximately 14.7 kN ⓘ
General Electric CF34-10E	approximately 20,000 lbf ⓘ
Snecma M53	around 64 kN dry ⓘ
Snecma M53	around 95 kN with afterburner ⓘ
Rolls-Royce RB211	around 37,000 to over 60,000 lbf ⓘ
Allison J35 turbojet surface form: Allison J35	around 4,000 lbf ⓘ
Allison J35 turbojet surface form: Allison J35	around 18 kN ⓘ
Rolls-Royce Pegasus turbofan surface form: Rolls-Royce Pegasus	around 20,000 to 24,000 lbf dry ⓘ
Rolls-Royce Adour turbofan surface form: Rolls-Royce Adour	approximately 5,000–6,500 lbf dry ⓘ
Rolls-Royce Adour turbofan surface form: Rolls-Royce Adour	approximately 7,000–8,000 lbf with afterburner (reheat) in some variants ⓘ
General Electric F404	approximately 48 kN dry thrust ⓘ
General Electric F404	approximately 79 kN thrust with afterburner ⓘ
Honeywell F124	approximately 6,000 lbf ⓘ
General Electric F414-GE-400	approximately 22,000 lbf with afterburner ⓘ
Pratt & Whitney PW2000	37,000 lbf ⓘ
Pratt & Whitney PW2000	40,000 lbf ⓘ
Pratt & Whitney PW4000 surface form: PW4000-94	52,000–62,000 lbf ⓘ
Pratt & Whitney PW4000 surface form: PW4000-100	64,000–70,000 lbf ⓘ
Pratt & Whitney PW4000 surface form: PW4000-112	74,000–99,000 lbf ⓘ
Rolls-Royce Nene engine surface form: Rolls-Royce Nene	around 5,000 lbf ⓘ
Rolls-Royce Nene engine surface form: Rolls-Royce Nene	approximately 22 kN ⓘ
Rolls-Royce Avon engine surface form: Rolls-Royce Avon	approximately 6,500–12,000 lbf dry ⓘ
Rolls-Royce Avon engine surface form: Rolls-Royce Avon	up to around 16,000 lbf with afterburner ⓘ
General Electric F414-GE-100	approximately 22,000 lbf with afterburner ⓘ
General Electric F414-GE-100	approximately 98 kN with afterburner ⓘ
Rolls-Royce Trent 1000	53000 to 78000 lbf ⓘ
General Electric GEnx	approximately 53,000 to 75,000 pounds-force ⓘ
Rolls-Royce Conway engine surface form: Rolls-Royce Conway	approximately 15,000–21,000 lbf depending on variant ⓘ
Heinkel HeS 3 jet engine surface form: Heinkel HeS 3	low thrust early turbojet ⓘ
Klimov RD-33 turbofan surface form: Klimov RD-33	about 50 kN dry thrust ⓘ
Klimov RD-33 turbofan surface form: Klimov RD-33	about 80–83 kN thrust with afterburner ⓘ
Pratt & Whitney F100 turbofan surface form: Pratt & Whitney F100	approximately 23,000–29,000 lbf with afterburner ⓘ
Heinkel HeS 011 jet engine surface form: Heinkel HeS 011	approximately 1300 kgf ⓘ
Heinkel HeS 011 jet engine surface form: Heinkel HeS 011	approximately 12.7 kN ⓘ
Pratt & Whitney J57	>10,000 lbf ⓘ
General Electric F118	about 17,000 lbf ⓘ
General Electric F118	about 75 kN ⓘ
General Electric F110 turbofan surface form: General Electric F110	approximately 28,000 lbf with afterburner ⓘ
General Electric F110 turbofan surface form: General Electric F110	approximately 29,000 lbf with afterburner ⓘ
General Electric F110 turbofan surface form: General Electric F110	approximately 32,000 lbf with afterburner ⓘ
Volvo RM12 turbofan surface form: Volvo RM12	approximately 80 kN with afterburner ⓘ
Volvo RM12 turbofan surface form: Volvo RM12	approximately 54 kN dry ⓘ
Turbo-Union RB199	approximately 40 kN dry ⓘ
Turbo-Union RB199	approximately 70 kN with afterburner ⓘ
Rolls-Royce Trent 700	around 60,000 to 72,000 lbf ⓘ